# N14952: 1998 Embraer EMB-145LR, registration cancelled 2015-10-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 5, 2015 - Exported to: Mexico - Status when cancelled: Valid registration - Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212) - Engine: [Allison AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145067 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 16, 1998 - Certificate issued: September 25, 2015 - Last registry action: September 25, 2015 - Mode S code: A0C741 - Owner when cancelled: [Spectre Air Capital LLC](https://openairdocs.org/faa-owner/SPECTRE%20AIR%20CAPITAL%20LLC) - Location: [Horseshoe Bay, TX](https://openairdocs.org/faa-place/TX/Horseshoe%20Bay) - Owner type: Corporation - Owner's area on the map: 30.5258° N, 98.3759° W: Placed by OpenAirDocs at the center of ZIP code 78657, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N14952 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14952 - Page: https://openairdocs.org/deregistered/N14952-2015-10-05 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Embraer EMB-145LR: https://openairdocs.org/model/embraer-emb-145lr.md ## Service difficulty reports (109, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20141120093](https://openairdocs.org/sdr/ASOA20141120093), Nov 20, 2014: LIGHT. FAULTY. THE CREW REPORTED THE EMERGENCY FLOOR LIGHTS WERE INOPERATIVE AT ROWS 3-18. MAINTENANCE INSPECTED AND REPLACED THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT. OPS CH - [SDR ASOA20141117131](https://openairdocs.org/sdr/ASOA20141117131), Nov 17, 2014: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION THE FWD RT SIDE EMERGENCY EXIT SIGN WAS DISCOVERED INOPERATIVE. MX R & R THE EMERGENCY LIGHT SYSTEM BATTERY CHARGER WITH OPS, GOOD - [SDR ASOA20140906095](https://openairdocs.org/sdr/ASOA20140906095), Sep 6, 2014: UNKNOWN. SMOKE. CREW REPORTED SMOKE COMING FROM LIGHT CONTROL PANEL ON F/O'S SIDE. MAINTENANCE INSPECTED BEHIND F/O'S LIGHT CONTROL PANEL AND OTHER PANELS IN THE VICINITY AND C - [SDR ASOA20140824092R](https://openairdocs.org/sdr/ASOA20140824092R), Aug 24, 2014: BATTERY PACK. DISCHARGED. CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT STAY ON DURING F/A TEST. MAINTENANCE CHARGED EMERGENCY LIGHT SYSTEM BATTERIES AND OPS CHECKED GOOD. ACFT WAS APPROV - [SDR ASOA20130809092R](https://openairdocs.org/sdr/ASOA20130809092R), Aug 9, 2013: UNKNOWN. ODOR. PILOT REPORTED A STRONG EXHAUST/FUEL ODOR IN FLIGHT DECK AND CABIN THROUGHOUT FLIGHT. MX RAN THE ENGINES AND APU WITH NO FUEL OR EXHAUST ODOR NOTED. ACFT WAS AP - [SDR ASOA20130420290](https://openairdocs.org/sdr/ASOA20130420290), Apr 20, 2013: LIGHT. INOPERATIVE. ACFT WAS IN FOR A LINE CHECK WHEN INSPECTION FOUND A FLOOR PROXIMITY LIGHT STRIP INOPERATIVE BETWEEN ROLL 2 THRU5. MAINTENANCE REMOVED AND REPLACED THE EMERGENC - [SDR ASOA20121213149](https://openairdocs.org/sdr/ASOA20121213149), Dec 13, 2012: DOOR FRAME. CORRODED. DURING C-CHECK LT OVERWING EMERGENCY EXIT LOWER FRAME CORRODED UNDER TEFLON GUIDE. MAINTENANCE PERFORMED AND COMPLETED REPAIR AT LT OVERWING EMERGENCY EXIT LOWE - [SDR ASOA20121213148](https://openairdocs.org/sdr/ASOA20121213148), Dec 13, 2012: SHEAR TIE. CORRODED. DURING C-CHECK SHEAR TIE AT FRAME 68 CORRODED. MAINTENANCE PERFORMED AND COMPLETED REPAIR AT FRAME 68 BY INSTALLING DOUBLER AND FILLER IAW EC 5320-01494. THE AC - [SDR ASOA20121213147](https://openairdocs.org/sdr/ASOA20121213147), Dec 13, 2012: FRAME. CORRODED. DURING C-CHECK, FRAME 65 CORRODED, IN UPPER RADIUS AT STRINGER 17L AND AT NUT PLATES FOR GUIDE. MAINTENANCE COMPLETED REPAIR AT FRAME 65 STRINGER 17L IAW EC5330 - [SDR ASOA20121213146](https://openairdocs.org/sdr/ASOA20121213146), Dec 13, 2012: STRINGER. CORRODED. DURING C-CHECK, STRINGER 20L CORRODED, AROUND RIVETS (2 EA) BETWEEN FRAMES 65-66. MAINTENANCE COMPLETED STRINGER REPAIR AT FRAMES 65-66 STRINGER 20L IAW SRM 53- - [SDR ASOA20121213145](https://openairdocs.org/sdr/ASOA20121213145), Dec 13, 2012: SILL. CORRODED. DURING C-CHECK, CARGO DOOR SILL CORRODED, FROM FRAME 65 TO 68. MAINTENANCE R & R CARGO DOOR SILL AT FRAMES 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RET - [SDR ASOA20121213144](https://openairdocs.org/sdr/ASOA20121213144), Dec 13, 2012: SHEAR TIE. CORRODED. DURING C-CHECK, SHEAR TIE CORRODED, FRAME 65, STRINGER 17L. MAINTENANCE COMPLETED SHEAR TIE SPLICE REPAIR AT FRAME 65, STRINGER 17L IAW EC5320-01494, REV A. THE - [SDR ASOA20120906074](https://openairdocs.org/sdr/ASOA20120906074), Sep 6, 2012: WIRE HARNESS. FAULTY. THE CREW REPORTED A STRONG ELECTRICAL ODOR IN CABIN. 17A CEILING LIGHT WAS INOPERATIVE. MX REPLACED ROW 17A CEILING LIGHT ELECTRICAL HARNESS ASSY. OPS CHECKS WE - [SDR ASOA20120507044](https://openairdocs.org/sdr/ASOA20120507044), May 7, 2012: CHARGER. FAULTY. DURING ROUTINE MX THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER AND EMERGENCY LIGHT B - [SDR ASOA20111215009](https://openairdocs.org/sdr/ASOA20111215009), Dec 8, 2011: CONDITIONER. FAULTY. AFTER TAKEOFF, IN CLIMB CREW REPORTED FUEL QTY NR1 WENT TO DASHES AND FUEL QUANITY NR 2 READ 0 LBS. CREW PERFORMED AIR RETURN WITHOUT ISSUE. MX R & R FUEL CONDI - [SDR C2XA11IA255](https://openairdocs.org/sdr/C2XA11IA255), Nov 8, 2011: SMOKE DETECTOR. MALFUNCTIONED. MCI - THE LAV SMOKE DETECTOR WAS REPORTED AS MALFUNCTIONING. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AN - [SDR C2XA11CL223](https://openairdocs.org/sdr/C2XA11CL223), Oct 4, 2011: UPLOCK. FAILED. THE CREW REPORTED IMMEDIATELY AFTER TAKEOFF FROM CLE A LOUD REPETITIVE THUMPING NOISE FROM UNDER THE AIRCRAFT. MOMENTARILY THE LEFT MAIN GEAR INDICATED AMBER CR - [SDR C2XA11IA201](https://openairdocs.org/sdr/C2XA11IA201), Sep 6, 2011: WINDOW. MALFUNCTIONED. IAH - FLIGHT 4586, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE CAPTAINS DV WINDOW WOULD NOT OPEN. MAINTENANCE INSPECTED THE AIRCRAFT AND VERIFIED NOR - [SDR C2XA11TY131](https://openairdocs.org/sdr/C2XA11TY131), Aug 20, 2011: LIGHT. BLOWN. TYS - A/C WAS IN FOR A ROUTINE CHECK WHEN INSPECTION FOUND THE EMERGENCY LIGHT BLOWN ON THE RIGHT OVERHEAD WING. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSE - [SDR C2XA11CL174](https://openairdocs.org/sdr/C2XA11CL174), Jul 25, 2011: SWITCH. FAULTY. CLE FLT 2431 THE CREW REPORTED A BLEED 2 VALVE CLOSED MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND - [SDR C2XA11CL167](https://openairdocs.org/sdr/C2XA11CL167), Jul 16, 2011: DUCT. LEAKING. ORD FLT 6187 THE CREW REPORTED A BLEED 1 LEAK MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE. MAINTENANCE REPLACED THE BLEED LINE O-RINGS AT JOINT 5, 9, 11, - [SDR C2XA11CL169](https://openairdocs.org/sdr/C2XA11CL169), Jul 15, 2011: BATTERY. OVERTEMP. ORD FLT 5854 THE CREW REPORTED A BATTERY NR 1 OVERTEMP MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. - [SDR C2XA11CL121](https://openairdocs.org/sdr/C2XA11CL121), May 12, 2011: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE THE AISLE PATH EMERGENCY LIGHT STRIPS NR 3 AND NR 4 WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ST - [SDR C2XA11TY042](https://openairdocs.org/sdr/C2XA11TY042), Apr 6, 2011: BATTERY. DISCHARGED. FLOOR PROX LIGHTS NR 1 2 & 3 ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04 OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO S - [SDR C2XA11IA063A](https://openairdocs.org/sdr/C2XA11IA063A), Mar 26, 2011: ACM. INOPERATIVE. MTY - FLIGHT 2127, THE CREW REPORTED THAT THE NUMBER ONE PACK WAS SURGING AND THE CABIN FILLS WITH SMOKE. PACK ONE WAS PLACED ON MEL, AND THE AIRCRAFT SUBSEQUEN - [SDR C2XA11TY018](https://openairdocs.org/sdr/C2XA11TY018), Feb 25, 2011: SKIN. DENTED. TYS - A/C HAD A DENT IN A PRIEVIOUS REPAIR AND TO MAY IN 1 AREA BETWEEN FR19 AND FR 20 AND STR 15L AND WAS PLACED ON 750 FLIGHT CYLE DMI. MAINTENANCE REMOVED AN - [SDR C2XA11IA023](https://openairdocs.org/sdr/C2XA11IA023), Jan 25, 2011: PROBE. INOPERATIVE. HOU - FLIGHT 2636 THE CREW REPORTED THAT THE NR 2 FUEL QUANTITY INDICATION DASHED OUT. THE AIRCRAFT DIVERTED TO HOU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANC - [SDR C2XA10IA311](https://openairdocs.org/sdr/C2XA10IA311), Nov 22, 2010: WIRE. BURNED. MTY - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT SIDEWALL LIGHT AT 9A TO BE SMOKING. MAINTENANCE PLACED THE SIDEWALL LIGHT IN MEL, AND THE AIRCRAFT WAS - [SDR C2XA10TY180](https://openairdocs.org/sdr/C2XA10TY180), Nov 17, 2010: LIGHT. INOPERATIVE. TYS - EMERGENCY FLOOR LIGHTS AT ROWS 6 AND 12 INOP. REMOVED AND REPLACED ROW 6 AND ROW 12 EMERGENCY LIGHT STRIPS, OPS CHECK GOOD. - [SDR C2XA10TY177](https://openairdocs.org/sdr/C2XA10TY177), Nov 16, 2010: SKIN. DENTED. TYS - DENT ON PREVIOUS REPAIR BETWEEN FRAMES 19 AND 20 STRINGER 15L. REPAIRED DENTS IAW EC5330-02287. - [SDR C2XA10TY175](https://openairdocs.org/sdr/C2XA10TY175), Nov 16, 2010: DOOR FRAME. CORRODED. TYS - A/C IS CURRENTLY IN A C-CHECK STATUS WHEN THE INSPECTION DEPARTMENT FOUND CORROSION UNDER THE LOWER AFT SERVICE DOOR TEFLON GUIDE. MAINTENANCE REPAIRED TH - [SDR C2XA10TY174](https://openairdocs.org/sdr/C2XA10TY174), Nov 16, 2010: FAIRING. DAMAGED. TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RIGHT SIDE HORIZIONTAL STAB TIP FAIRING WITH MULTIBLE SPOTS OF DAMAGE COMPOSITE. MAINTENANCE REPAIRED T - [SDR C2XA10TY173](https://openairdocs.org/sdr/C2XA10TY173), Nov 16, 2010: BRACKET. WORN. TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RIGHT AILERON PCA BRACKET OUTBOARD HAT BUSHION HOLE OUT OF LIMITS. MAINTENACE REMOVED AND REPLACED THE - [SDR C2XA10TY176](https://openairdocs.org/sdr/C2XA10TY176), Nov 15, 2010: SKIN. CORRODED. TYS - LOWER SKIN CORRODED AT FR14 BETWEEN STR 19L AND 19R. REMOVED AND REPLACED SKIN IAW EC5330-02280. - [SDR C2XA10TY172](https://openairdocs.org/sdr/C2XA10TY172), Nov 15, 2010: STRINGER SPLICE. CORRODED. TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE STRINGER SPLICE CORRODED AT STRINGER 20R AND FRAMES 13-14. MAINTENANCE REMOVED AND REPLACED TH - [SDR C2XA10RI117](https://openairdocs.org/sdr/C2XA10RI117), Sep 14, 2010: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 2348 - EWR - FLIGHT CREW REPORTED LANDING GEAR LEVER DISAGREE MESSAGE ON EICAS. FLIGHT CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX PER - [SDR C2XA10IA198](https://openairdocs.org/sdr/C2XA10IA198), Jul 8, 2010: UNKNOWN. ODOR. IAH - FLIGHT 2973 THE CREW REPORTED A FUEL SMELL IN THE COCKPIT WHEN ANTI-ICE CAME ON AND ON DESCENT. IT WAS NOTED THAT THE SMELL DISSIPATED QUICKLY. THE AIRCRA - [SDR C2XA10RI037](https://openairdocs.org/sdr/C2XA10RI037), Mar 15, 2010: DOOR. LACK OF LUBE. FLIGHT 2892 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR VERY DIFFICULT TO OPEN. EWR MX LUBRICATED MAIN CABIN DOOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. - [SDR C2XA09CL074](https://openairdocs.org/sdr/C2XA09CL074), May 26, 2009: TURBINE WHEEL. CRACKED. DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND DURING THE ULTRASOUND INSPEC - [SDR C2XA09CL041](https://openairdocs.org/sdr/C2XA09CL041), Apr 8, 2009: TUBE. LEAKING. DURING ROUTINE MAINTENANCE THE PRESSURE REFUEL/DEFUEL LINE WAS FOUND LEAKING. MAINTENANCE INSPECTED AND FOUND THE TUBE ASSEMBLY TO BE CORRODED. THE TUBE WAS REP - [SDR C2XA08RI182](https://openairdocs.org/sdr/C2XA08RI182), Dec 18, 2008: CLAMP. DEFORMED. FLIGHT 2775 - EWR - FLIGHT CREW REPORTED ENG NR 1 BLEED LEAK INDICATION ON EICAS IN FLIGHT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX R&R BLEED - [SDR C2XA08RI180](https://openairdocs.org/sdr/C2XA08RI180), Dec 15, 2008: SWITCH. INOPERATIVE. FLIGHT 2306 - EWR - DURING CLIMBING FLIGHT CREW REPORTED THE FOLLOWING MSGS ON EICAS: PACK 2 CLSD AND BLD 2 CLSD. CREW RESET THE SYSTEM BUT FAILED AGAIN AND WHE - [SDR C2XA08RI179](https://openairdocs.org/sdr/C2XA08RI179), Dec 15, 2008: BLEED VALVE. INOPERATIVE. FLIGHT 2306 EWR DURING CLIMBING FLIGHT CREW REPORTED THE FOLLOWING MSGS ON EICAS: PACK 2 CLSD AND BLD 2 CLSD. CREW RESET THE SYSTEM BUT FAILED AGAIN AND WHEN TR - [SDR C2XA08SH145](https://openairdocs.org/sdr/C2XA08SH145), Nov 11, 2008: ATTACH BRACKET. WORN. SHV - DURING C-CHECK THE RUDDER UPPER CENTER ATTACHMENT BRACKET WAS FOUND TO BE WORN AND THE HAT BUSHINGS MIGRATED. MAINTENANCE REMOVED AND REPLACED THE AFFECTE - [SDR C2XA08SH144](https://openairdocs.org/sdr/C2XA08SH144), Nov 11, 2008: SILL. CORRODED. SHV - DURING C-CHECK THE CARGO DOOR LOWER CUTOUT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE - [SDR C2XA08SH143](https://openairdocs.org/sdr/C2XA08SH143), Nov 11, 2008: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 - [SDR C2XA08SH142](https://openairdocs.org/sdr/C2XA08SH142), Nov 11, 2008: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 34. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 - [SDR C2XA08SH141](https://openairdocs.org/sdr/C2XA08SH141), Nov 11, 2008: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR I - [SDR C2XA08SH140](https://openairdocs.org/sdr/C2XA08SH140), Nov 8, 2008: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CORROSION ON LT OMEGA BEAM JUST ABOVE FR 20 CARBON CROSS BEAM. MX REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10 FIG 201. THE AIR - [SDR C2XA08SH139](https://openairdocs.org/sdr/C2XA08SH139), Nov 8, 2008: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CORRODED NUT PLATE HOLE ON OMEGA BEAM LAV AREA BETWEEN FRAME 60 AND 61 LT SIDE. REPAIRED LT OMEGA BEAM BETWEEN FR 60-61 AT NUT PLATE ARE IA All 109: https://openairdocs.org/deregistered/N14952-2015-10-05/reports.md ## Other aircraft with N14952 - [Cancelled 1936-04-21](https://openairdocs.org/deregistered/N14952-1936-04-21): Ryan Aeronautical ST-A, S/N 108. Owner: [Dods James (Estate)](https://openairdocs.org/faa-owner/DODS%20JAMES%20(ESTATE)), [Honolulu, HI](https://openairdocs.org/faa-place/HI/Honolulu) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.